FLIGHT CREW OPERATIONS MANUAL SUPPLEMENT STA … · Preface Chapter 0 Introduction Section 1 0.4...

This Flight Crew Operations Manual Supplement is incomplete without theBoeing Flight Crew Operations Manual. The document contained hereinsupplements or supersedes the information given in the Flight CrewOperations Manual Document D632N001 for airplanes modified in

FCOM Supplement for Boeing757-200 with STA Mobile

Combi Freighter ModificationDocument No. : 757SC-FCOM-01

Revision : 4Issue Date : November 12, 2013

FLIGHT CREW OPERATIONS MANUAL SUPPLEMENTSTA MOBILE COMBI FREIGHTER MODIFICATION

: BOEING

: 757-200AIRPLANE MODEL

AIRPLANE MAKE

2100 9TH STREET BROOKLEY COMPLEX, MOBILE, AL36615, USAST Aerospace Mobile, Inc.

AIRPLANE REGISTRATION NO. : __________

AIRPLANE SERIAL NO. : __________

accordance with Supplemental Type Certificate __________.

757 Flight Crew Operations Manual Supplement

Preface Chapter 0Table of Contents Section 0

0.0 Preface-Table of ContentsVolume 1 ChapterPreface

Table of Contents .................................................................................0.0

Revision Record...................................................................................0.2List of Effective Pages .........................................................................0.3

Volume 2 Airplane General, Emergency Equi

0.0.S1December 02, 2011 757SC-FCOM-01

(Applicable for 757 Combi Freighter Aircraft)

........................................................................................................0

Introduction......................................................................................... 0.1

Limitations ................................................................................................LNormal Procedures................................................................................. NPSupplementary Procedures......................................................................SP

pment, Doors, Windows ....................1Air Systems ............................................................................................... 2Fire Protection........................................................................................... 8Hydraulics ................................................................................................13Warning Systems .....................................................................................15

Preface -Table of Contents

Quick Reference Handbook (QRH)EICAS Index

0.0.S2 December 02, 2011


757SC-FCOM-01


.......................................................................EICAS.IndexAlphabetical Index................................................................ Alpha.IndexNon–Normal Checklists ...................................................................NNC

Preface Chapter 0Introduction Section 1

0.4 Preface-Revision Record


0.1.S1757SC-FCOM-01

GeneralThis Flight Crew Operations Manual Supplement has been prepared by STAerospace Mobile, for airplanes modified in accordance with SupplementalType Certificate __________. The purpose of this supplement is to provide theoperating limitations, procedures and systems information the flight crew needsto operate the modified 757 airplane.This supplement is to be used in conjunction with the latest revision of the 757Flight Crew Operations Manual (FCOM), Boeing Document Number: D632N001for the specific airplane.

Questions about the contents or use of this manual can be directed to:

Attn: Director, Engineering

The pages are to append to the corresponding pages wherever the contents areamended. Where the page numbers are unique (Example: page 8.2A), the pagesare to be inserted opposite the existing page (in the example page 8.2).

2100 Aerospace Drive

Mobile, AL 36615Street Brookley Complex

ST Aerospace Mobile, Inc.

USA


For the Quick Reference Handbook (QRH), the pages are to replace thecorresponding pages wherever the contents are amended. Where the pagenumbers are unique (Example: 8.15A), the pages are to be inserted immediatelyafter the existing page (in the example 8.15).

December 02, 2011

Preface Chapter 0Revision Record Section 2

0.4 Preface-Revision RecordRevision Transmittal LetterTo: All holders of 757 Flight Crew Operations Manual (FCOM), for airplanesmodified in accordance with Supplemental Type Certificate __________.Subject: Flight Crew Operations Manual Supplement.This supplement reflects the modification made by ST Aerospace Mobilein converting it into a combi freighter airplane. The following revisionhighlights explains changes in this revision. The Revision Record page explainsthe use of revision bars to identify new or revised information.


0.2.S1

Revision Record

GeneralST Aerospace Mobile issues FCOM supplement revisions to provide new orrevised procedures and information.

The revision date is the approximate date the manual is issued to the customer and is effective upon receipt.Formal revisions include a Transmittal Letter, a new Revision Record, Revision Highlights, and a current List of Effective Pages. Use the information on the new Revision Record and List of Effective Pages to verify the FCOM content.Pages containing revised material have revision bars and highlights associated with the changed text or illustration. Revision bars associated with revised effectivity due to additions, deletions of airplanes or changes to previous registration numbers will not have highlights.The record should be completed by the person incorporating the revision into the manual.

No. Revision Date Date Filed

0 December 2, 2011

No. Revision Date Date Filed

757SC-FCOM-01November 12, 2013


1 December 23, 2011

3 August 28, 2012

4 November 12, 2013

2 January 20, 2012

Preface -Revision Record

Filing InstructionsConsult the List of Effective Pages (0.3). Pages identified with an asterisk (*) are either replacement pages or new (original) issue pages. Remove corresponding old pages and replace or add new pages. Remove pages that are marked DELETED; there are no replacement pages for deleted pages.

Be careful when inserting changes not to throw away pages from the manual that are not replaced. The List of Effective Pages determines the correct content of the manual.

Pages marked with a letter such as 'A' are to be inserted opposite the said page.


0.2.S2 757SC-FCOM-01

Revision Highlights

November 12, 2013


Chapter SP - Supplementary ProceduresSP.1.1A - Updated Main Cargo Door Closing procedures.

SP.1.1B - Updated Main Cargo Door Opening procedures.

Chapter NP - Supplementary ProceduresNP.21.10A - Added Main Deck Cargo Door Visual Inspection as required.

Quick Reference Handbook1.2 - Revised procedures for CARGO DOOR(S) in Non-Normal Checklist.

Chapter 1 - Airplane General, Emergency Equipment, Doors, Windows1.30.14A - Updated description of CANOPY POSITION light.

PrefaceList of Effective Pages

Chapter 0

Section 3

* = Revised, Added, or Deleted

0.5 Preface-List of Effective Pages


Page Date

Volume 2

1 Airplane General, Emergency Equipment, Doors, Windows (tab)

2 Air Systems (tab)

1.TOC.0.1A

2.TOC.0.1A

1.20.2A

1.21.4A

0.3.S1757SC-FCOM-01

1.20.3A

1.30.11A1.30.14A

1.40.6A1.40.7A1.40.9A1.40.12A1.40.13A

1.50.1A

2.10.1A 2.10.3A 2.10.10A2.20.1A2.20.2A2.20.3A2.20.4A2.20.5A

1.45.3A1.45.4A

November 12, 2013


1.22.3A

December 23, 2011

August 28, 2012December 02, 2011December 02, 2011December 02, 2011December 02, 2011December 02, 2011

December 02, 2011December 02, 2011December 02, 2011December 02, 2011December 02, 2011December 02, 2011

August 28, 2012

December 02, 2011December 02, 2011December 02, 2011December 02, 2011December 02, 2011December 02, 2011December 02, 2011December 02, 2011December 02, 2011

0.5 Preface-List of Effective PagesPage Date

Volume 1

Preface

Limitations

Normal Procedures (tab)

Supplementary Procedures (tab)

Title Page

L.10.5A

L.TOC.0.1A

SP.TOC.0.1ASP.1.1ASP.1.1B

SP.15.1ASP.16.12A

0.0.S1

SP.8.1A

NP.21.14ANP.21.10A

0.1.S10.2.S1

0.3.S2

0.0.S2

0.2.S2

0.3.S1

*

*

*

0.2.S3

0.2.S4

L.10.3A

December 02, 2011

Deleted

December 23, 2011

Deleted

December 02, 2011December 02, 2011

December 02, 2011December 02, 2011December 02, 2011

November 12, 2013December 02, 2011

December 02, 2011

November 12, 2013November 12, 2013


August 28, 2012

January 20, 2012

November 12, 2013* *

1.30.14B August 28, 2012

NP.21.14A December 02, 2011

November 12, 2013

November 12, 2013

* November 12, 2013

Preface -List of Effective Pages

* = Revised, Added, or Deleted

0.3.S2


8 Fire Protection (tab)

Page Date

13 Hydraulics (tab)

15 Warning Systems (tab)

13.TOC.0.1A

15.20.10A15.30.2A

Page Date

Quick Reference Handbook

757SC-FCOM-01

8.10.3A8.10.3B8.10.3C

8.20.4A8.20.5A8.30.1A

13.20.1A13.20.2A13.20.3A13.20.4A

EICAS.Index.6

EICAS.Index.8Alpha.Index.3

1.22.182.197.36

8.15A8.15B

8.TOC.0.1A

Alpha.Index.4Alpha.Index.10

15.2

November 12, 2013

December 02, 2011


EICAS.Index.6AEICAS.Index.6B

Alpha.Index.13

8.TOC.18.138.15

8.1715.TOC.1

1.TOC.1*

December 23, 2011



December 02, 2011December 02, 2011December 02, 2011December 02, 2011December 02, 2011


December 02, 2011December 02, 2011December 02, 2011December 02, 2011December 02, 2011December 02, 2011December 02, 2011December 02, 2011

November 12, 2013December 02, 2011December 02, 2011December 02, 2011December 02, 2011December 02, 2011

December 02, 2011December 02, 2011December 02, 2011December 02, 2011

January 20, 2012January 20, 2012


757SC-FCOM-01L.TOC.0.1A

Limitations Chapter LTable of Contents Section 0

L.0 Limitations-Table of Contents

Operating Limitations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . L.10


Main Cargo Door . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . L.10.5A

December 02, 2011


757SC-FCOM-01

Limitations -Operating Limitations

L.10.3A

Maximum Weight Limitations

Other Weight Restrictions

Note: These weights may be further restricted by field length limits, climb limits, tire speed limits, brake energy limits, obstacle clearance, or enroute and landing requirements.

Door Mounted Escape SlidesEntry door evacuation slide systems must be armed and engagement of the girt bar with door sill verified prior to taxi, takeoff, or landing whenever passengers orsupernumeraries are carried.

Weights Kilograms

Maximum Taxi Weight (MTW) 116,074

Maximum Landing Weight (MLW) 90,718

Maximum Weight LimitationsOO-TFA

Maximum Take Off Weight (MTOW) 115,666

Maximum Zero Fuel Weight (MZFW) 83,460

(Applicable for 757 Combi Freighter Aircraft)December 02, 2011


757SC-FCOM-01

Limitations -Operating Limitations

L.10.5A

Main Cargo DoorMaximum allowable wind speed at the main cargo door is 40 knots for dooroperation and 60 knots with the door open.


NP.21.10A

Normal Procedures -Amplified Procedures


757SC-FCOM-01

(Applicable for 757 Combi Freighter Aircraft)November 12, 2013

Main Cargo Door

Main Cargo Door ............................................ Closed, latched & locked

Verify that the vent door is closed. (For night operation, a flashlight is necessary for this check.)

NP.21.13A


MAIN CARGO FIRE SUPPRESSION panel .....................................Set

Verify that the BTL DSCH light is extinguished


757SC-FCOM-01

ARM switch – OFF

Verify that the BTL lights are extinguished

HEATER switch – As desired

COURIER AREA TEMPERATURE CONTROL panel ....................Set

TEMP IND switch – As desired

Verify that the FIRE light is extinguished


NP.21.14A


Verify that the FWD and MID FIRE lights are extinguished.

MAIN FIRE panel .............................................................................. Set


Verify that the fault lights are extinguished.

757SC-FCOM-01

Right recirculation fan is removed on the combi freighter.NOTE:

Verify that the Loop switches are selected to BOTH.

LEFT RECIRCULATION FAN switch – ON


Supplementary Procedures Chapter SPTable of Contents Section 0

Airplane General, Emergency Equipment, Doors, Windows . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SP.1

Doors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SP.1.1Main Cargo Door Closing . . . . . . . . .

. . . . . . . . . . . . . . . . . . SP.1.1B. . . . . . . . . . . . . . . . . . . SP.1.1A

Main Cargo Door Opening . . . . . . .


SP.TOC.0.1A 757SC-FCOM-01


Fire Protection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SP.8

Main Deck Fire Detection Test. . . . . . . . . . . . . . . . . . . . . . . . . . . SP.8.1AMain Deck Cargo Compartment Fire Suppression System Test. . SP.8.1A

December 02, 2011

SP.1.1A

Chapter SPSupplementary ProceduresAirplane General, Emergency Equipment, Doors, Windows Section 1

Main Cargo Door ClosingDoor Area ............................................................................ Check Clear

Verify Arm light illuminatesDoor Control Switch .................................................. CLOSE and Hold

DR SYS will illuminate for several seconds during operation

Arming Switch ..........................................................................DISARMVerify Arm light extinguishes


757SC-FCOM-01

ARM/DISARM Switch ..................................................................ARM

Observe door closing from door 1L


When Main Cargo Door is fully closed, latched and locked,

• Green light illuminates; CLOSED, LATCHED AND LOCKED• Amber light is not illuminated, DR SYS

Verify on the Main Cargo Door indicating panel:• 4 red lights extinguish; NOT CLOSED, NOT LATCHED,

NOT LOCKED, VENT DR NOT CLOSED

SP.1.1B

Supplementary Procedures -Airplane General, Emergency Equipment, Doors, Windows

Main Cargo Door Opening

Door Area ............................................................................ Check Clear

Verify Arm light illuminates

Door Control Switch ...................................................... OPEN and HoldObserve door opening from door 1LDR SYS light will illuminate for several seconds during operation

Door Control Switch .............................................................. NEUTRAL

Verify Arm light extinguishes

CAUTION:knots or let the door stay open in winds more than 60Do not operate the cargo door in winds more than 40

knots. Strong winds can cause damage to the door andthe actuating mechanism.

commence immediately, fit the safety net across the doorIf cargo loading/unloading operations are not to

opening.

APU or External Power and Left Hydraulic Power is required to operate the Main Cargo Door.

NOTE:


757SC-FCOM-01

ARM/DISARM Switch .................................................................. ARM

ARM/DISARM Switch ............................................................ DISARM


When Main Cargo Door reaches desired opened position,

NOT LOCKED, NOT LATCHED, NOT CLOSED• Green light extinguishes; CLOSED, LATCHED AND LOCKED• Amber light is not illuminated, DR SYS

position.CANOPY POSITION light illuminates when the door is at canopy

Verify on the Main Cargo Door indicating panel:• 4 red lights illuminate; VENT DR NOT CLOSED,

SP.8.1A

Supplementary Procedures Chapter SPFire Protection Section 8


757SC-FCOM-01

Main Deck Fire Detection Test

MAIN FIRE System Test Switch................................................ PushObserve the aural warning from Main Cargo Smoke Alarm PanelObserve the following lights illuminate:

Discrete FIRE warningFWD, MID FIRE

Master WarningObserve the following EICAS message:

MAIN CARGO FIRE

FIRE Warning Light on Main Cargo Fire Suppression Panel

FIRE/OVHT SYS

Main Deck Cargo Compartment Fire Suppression System Test

Observe the following lights illuminate:BTL 1, 2, 3, 4 & 5 (Green)DSCH (Amber)

Main Cargo Fire Suppression Panel SYS TEST Switch..............Push

December 23, 2011


Supplementary Procedures Chapter SPWarning Systems Section 15

Takeoff Configuration Warning Test

Establish one or more of the following conditions:Flaps not in takeoff positionSpeedbrakes not downStabilizer units set greater than green bandPark brake set

Configuration Test switch .................................................................. T/OObserve CONFIG light illuminate, and appropriate configuration warning message(s) display.

Establish appropriate configuration.

SP.15.1A

Main cargo door not closed, latched and locked


757SC-FCOM-01


SP.16.12A

Supplementary Procedures -Adverse Weather

Hot Weather OperationNote: Right recirculation fan is removed on the combi freighter.


757SC-FCOM-01


1.TOC.0.1A

Airplane General, EmergencyEquipment, Doors, Windows -

Table of Contents757 Flight Crew Operations Manual Supplement

757SC-FCOM-01

Chapter 1Airplane General, Emergency Equipment, Doors, WindowsTable of Contents Section 0

1.30.10


Main Cargo Door Control Panel . . . . . . . . . . . . . . . . . . . . . 1.30.14A

Rigid Cargo Barrier Door . . . . . . . . . . . . . . . . . . . . . . . . . . 1.40.9ASmoke Barrier Door . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.40.9A

Doors and Windows . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Main Cargo Door Indicator . . . . . . . . . . . . . . . . . . . . . . . . . 1.30.11A

Cargo Door Area Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.40.6A

Controls and Indicator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.30

System Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.40

1.40.7Doors and Windows . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

1.40.1Lighting Systems . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

August 28, 2011

Main Cargo Door Indicating Panel . . . . . . . . . . . . . . . . . . . 1.30.14B

Left Overhead Panel

1.20.2A

Airplane General, Emergency Equipment, Doors, Windows -Instrument Panels, Overhead


757SC-FCOM-01

9 9 14

9 9 9

3 3 3

3 3 3

9

3

1 1 1 1

L C R

ATT

HIGH

OFF

LOW

WIPER

UNARMED

ON

EMER LIGHTS PASS OXY

ARMED

OFF

ON

R

R

LENGINE

ANTI-ICE

L

WING

VALVEVALVEVALVEVALVE

L

GND

RAM AIR TURB

FLT

CONTOFF

AUTO

PRESS

UNLKD

VALVEVALVE

BOTH1 2

ENG STARTR

GND

FLT

CONTOFF

AUTO

RSVR

SYSPRESS

RSVR

SYSPRESS

RSVR

SYSPRESS

HYD PUMPS

ENGR

- - 2ELEC1C

ENGL

OVHT

ELECELEC

PRESSPRESSPRESSPRESS

PRESS PRESS

OVHTOVHTOVHT

OVHT OVHT

RLYAW DAMPER

INOPINOP

FAULT

APUSTART

ONOFF

RUN

600 OHMSCOCKPIT VOICE RECORDER

HEADSET

ERASETEST

AUTOBAT

STBY POWER

OFF

FFO

BAT

OFF

SID

CH

IRS MODE SEL

N2 3

W4

H5

E6

7 S8 9

ENT 0 CLR

1

TK/GS

PPOSDSPL SEL

WIND

HDG

SYS DSPL

L C R

ALIGN

ON DC

DC FAIL

FAULT

ALIGN

ON DC

DC FAIL

FAULT

ALIGN

ON DC

DC FAIL

FAULT

ALIGN

OFF

NAV ATT ALIGN

OFF

NAV ATT ALIGN

OFF

NAV

FUEL QTYX 1000

L

TOTAL

C

TEMP 0F

LB LB LB

R

OFF

ISLN

AUTO

ISLN

AUTO

OFF OFF

APU GEN EXT PWR

BUSOFF

ON

AVAIL

BUSOFF

OFF

DRIVE

BUS TIE BUS TIE

UTILITY BUS

L R R BUSL BUS

LGEN

CONT

RGEN

CONTGEN DRIVE DISCL R

OFF DRIVE

RL

GLARESHIELD

RUNWAY TURNOFF

AISLE STANDPANEL/FLOOD

OFF

OFF

ON

LT OVRD

ANTISKID

DOORSENTRY

PITOTCAPT

PITOTL AUX

TRIMSTAB

STAB TRIMUNSCHED

DOORSEMER

PITOTF O

PITOTR AUX

SPOILERS

RATIORUDDER

DOORSCARGO

L AOA

TAT

R AOA

SPDBRKAUTO MACH

SPD TRIM

ACCESSDOORS

OFF AMUSB

RF SENS

FH

1

1

ANTICOLLISIONRED WHITE

LANDING

POSITION WING

WING NOSE GEARL R

OFF

ON

OFF

ON

PRESS

RL

C PUMPS

XFEEDFUEL R

PUMPSL

PUMPS

FWD

AFT

FWD

AFT

FUELCONFIG

PRESS

PRESS

PRESS VALVE

VALVE

PRESS

PRESS

ON

ONON ONON

ONON ON

ONON

ON

ON

ON ON

ON

ON ON

ONON ON ON

ON ON

ON ON

ON ON

65 13

ON

OFF

BRT

TEMP IND

FWDCOURHIGHOFF

HEATER

LOW

INOP

INOP

COURIER

ALARMOFF

1

7

12

3

1

6

7

5

1

11

9

13

8

2


MAIN CARGO SMOKE ALARM

December 02, 2011

Right Overhead Panel


Airplane General, EmergencyEquipment, Doors, Windows -Instrument Panels, Overhead

1.20.3A757SC-FCOM-01

PRESS DIFF

.125 PSITO/LDGLIMIT:

ALTITUDECABIN

01 2

21252015

10 8 64

2010

86

4

20

1000FPM X

1000FT X

PSIDIFF ALT RATE

CABIN

YBTS

W

NAUTO

OFF

RESET

OFFPACK

INOP

INOP

MODE SELECTAUTO 2

AUTO 1 MAN

LDG ALT

MIN MAXDESCEND

CLIMBMANUAL

AUTO RATEVALVE

OP

CL

CABIN ALTITUDE CONTROL

AUTO INOP00340

60 80

20 0

DUCTPRESS

PSI40

OFF AMUSB

RF SENS

FH

ONOFFAUTO

EQUIP COOLING

ALTN

OVHTSMOKE

NO SMOKINGPASS SIGNS

ONOFFAUTO

SEAT BELTS

ISOLATION

R ENG

VALVE

LEAKDUCT

BLEED

HI STAGE

LEAKDUCT

BLEED

HI STAGE

VAL

OFF

OFF V

E

APUL ENG

BLEED AIR

KCAP RKCAP L

OFFPACK

INOP

RESET

ON

INOPINOP

L RECIRCFAN

ON

OFF

TRIM AIR

YBTS

W

NAUTO

OFF

OFFWC

AUTO

FLT DK COUR/FWD AFT

FLT DK

OFFWC

AUTOFWD CAB

OFFWC

AUTOAFT CAB

INOP INOP

TEST

OFF

DENY

DOME

OFF

OVHD PANEL

OFF

CKT BKR

UNLKDAUTO

BRTDIMIND LTS

INOP AUTO

LOCKFAIL

UNLK

ON

LOGO FLT DK DOOR

ON

INOP

ON

INOP

WINDOW HEAT

SIDE FWDL

ON

INOP

ON

INOP

FWD SIDER COMPT TEMP

3

5 2

2

1

2

1

SYSTEM

FAULT

FWDBOTH

A B

FIRE

MAIN

FAULT

BOTHA B

FIRE

MIDBOTH

A B

DEACT

TEST

DEAC

T

DEAC

T

8 8

L

GNDCALL INT

FLT

bALERT

C/ACARSVHF

R L RHF

b b b bb

bb bb b

DEACT DEACT

DEACT DEACT DEACT DEACT

SELCAL

IRE

F

OFF

PUSHBTL

DSCH

BTL

3 54

21

DEACT


DEACT

DEACT

INOP

ARMED

ARM

SYS TEST

FIREMAIN CARGO FIRE

SUPPRESSION

BTL DSCH

December 02, 2011

1.21.4A

Airplane General, Emergency Equipment, Doors, Windows -Instrument Panels, Forward

Center Forward Panel


757SC-FCOM-01

AUTO

AUTO BRAKES

DISARMMAX

4

32

RTO

OFF

1BRAKESAUTO

N1

EGT

N2

EPR

.005

645

100

1

ONAUTO

.005

645

1

100

AUTOPILOT

FMC

ALERTALT

A/TDISC

SPEEDBRAKES

GND

OVSPD

CONFIG

CABIN

PULL UP

FIRE

A/P

ALT

DISC

CAUTION

RECALLCANCEL

ILSOFF

B/CRS

IAS

KNOTS

80100

120

140

60

160180

200220

240250

300

350400

8

IN. HG2

3

2

10

9

7

6 54

9 9 23101MB

BARO

40

50

60

30

20

10GMT

ET/CHR

DATE

MO/YRDAY

CHR

BRAKESRESERVE

ON

BRAKESOURCE

VALVE

1000 FPM.5

.5

OFF

1 2

4

VERTICALSPEED

1 2

4

60

MB IN.HG1013

4

ALT 3

6

8

9 0 1

2

59229

OFF

B RA O

ALT

MIDDLE

INNER/AIRWAYS

OUTER

AUTOLAND STATUS

P/RST1

2

TEST

NO

LAND 3

LAND 3

NORM30

5

UP

25

20

15

ALTN FLAPS

1

240K220K

210K

195K

190K162K

UPFLAPS

515

25

20

1

30

FLAP LIMIT IAS

TELE

ALTN ALTN GEAR OVRD

OVRD

FLAP OVRD

OVRD

GND PROXTERR OVRD

OVRD

250K-.75MEXTEND

ALTN GEAR

OFF

DN

270K

270K-.82MEXTENDEDEXTEND OR

DN

UP

OFF

RETRACT

LOCK OVRD

CON

TOGA

CRZ

CLB 1 2

TEMP SEL

LEADINGEDGE

TRAILINGEDGE

HDG REFNORM

TRUE 20

13

4BRAKEPRESS

1000XSP I

AUTOLAND STATUS

P/RST1

2

TESTLAND 2

NO AUTOLND

MACH

0

5

4KNOTS

7

2 4

3

DME-RDME-L

ROV

ROV

ADF ADF

ADF INOP

9

15

4

4

2

815

15

11

15

4

15

1

15

AND7 15

10

10 415

10

10 7

7 9

1

114

15

14

15

14

1410

18

DOORS

WHL WELLFIRE

NOSE

MN CARGODOOR G

EAR

RIGHTLEFT


1.22.3A

Airplane General, Emergency Equipment, Doors, Windows -Instrument Panels, Aft and Side


757SC-FCOM-01

Right Sidewall, Accessory Panel


INOPR

EQUIPYAW DMPR

PROBE HEATWINDOW/ FUEL

LLEAKDUCT

ANTI ICEWING

COOL

HYD GENLDG

GNDT/O

RSTALLL

CONFIGPROX

TEST

AIR DATACMPTRL R

QTY

TEST

APU

SQUIB TESTRENGL

2121

2121AFT FWDCARGO

DISPLAY SELECT

PERFELEC

APUHYDMSG

ECS

MCDP

CONF ENGEXCD

ERASERECTEST

AUTOEVENTREAD MAN

EICAS MAINT

ON

TEST

SERV INTPHFLT RCDR

ONNORM

OFFOFF

PTU

ON

L C R

OFFOFFOFF

OFF

ON

FLT CONTROL SHUTOFF

ON ON

HEADSET ANDSMOKE

STOWAGEGOGGLES

15

12

15

13

5

910

6

8

100%

OXYGENRESETTEST

PUSH

MASKN

MINUTES

30

0

4515

510

5550

3540

2520

1

December 02, 2011

1.30.11A


Controls and Indicators

Main Cargo Door Indicator

1 Main Cargo Door (MN CARGO DOOR) IndicatorIlluminated (red) - the Main Cargo Door is not closed, latched and locked.

INSTRUMENT PANEL

Exterior Door Locations

R FWD ENT DOORL FWD ENT DOOR

FWD CARGO DOOR

AFT CARGO DOOR

E/E ACCESS DOOR

FWD ACCESS DOOR

EICAS MESSAGE NOMENCLATURE USED FOR DOORS IDENTIFICATION

EXTERIOR DOORS

MAIN CARGO DOOR


757SC-FCOM-01

L EMER DOOR R EMER DOOR

L AFT ENT DOOR R AFT ENT DOOR

RIGHTLEFT

NOSE

MN CARGODOOR

WHL WELLFIRE

GEAR

DOORS

1




1.30.14A

4 CANOPY POSITION LightIlluminated (green) - the Main Cargo Door is at the canopy position.

COURIER AREA

MAIN CARGO DOOR CONTROL PANEL

CARGO AREA SwitchIlluminated (white) - the Main Cargo Door area and Main Deck Cargo

2

OPEN/CLOSE Control SwitchOPEN - opens the Main Cargo Door when armed.

3

NEUTRAL - stops the Main Cargo Door at its current position.CLOSE - closes the Main Cargo Door when armed.

WORK SwitchIlluminated (white) - the work lights are on.

5

ARM/DISARM SwitchARM (illuminated) - the Main Cargo Door opens/closes according to the controlswitch position.

6

DISARM (extinguished) - the Main Cargo Door remains locked at its currentposition.

4

5

62

3


757SC-FCOM-01

Compartment lights are on.


ENTRY

CARGO DRMANUAL

OPERATION

WORKTHRESHOLD

CANOPYPOSITION

GROUNDSERVICE

ARM/DISARMCARGOAREA

CLOSE

OPEN

CARGO DOOR CONTROL

OFF HI

1

CARGO DR MANUAL OPERATION SwitchIlluminated (amber) - the Main Cargo Door is enabled for manual operation.

1



1.30.14B

3 NOT LOCKED LightIlluminated (red) - the Main Cargo Door is not locked.

MAIN CARGO DOOR INDICATING PANEL

NOT CLOSED LightIlluminated (red) - the Main Cargo Door is not closed.

1

NOT LATCHED LightIlluminated (red) - the Main Cargo Door is not latched.

2

VENT DR NOT CLOSED LightIlluminated (red) - the Main Cargo Door's vent door is not closed.

4

CLOSED, LATCHED & LOCKED LightIlluminated (green) - the Main Cargo Door is closed, latched and locked.

5


757SC-FCOM-01

(Applicable for 757 Combi Freighter Aircraft)August 28, 2012

DR SYS LightIlluminated (amber) - when the Main Cargo Door is not operated, either there is

6

a hydraulic leakage in the Main Cargo Door and/or the Main Cargo Door switchsensors are in disagreement.

DR SYSCLOSEDLATCHED& LOCKED

VENT DRNOT CLOSED

NOTLOCKED

NOTLATCHED

MN CARGO DR IND

NOTCLOSED

1

3

5

2

4

6

Airplane General, Emergency Equipment, Doors, Windows -Systems Description

Interior Emergency LightingInterior emergency lighting consists of door, aisle, exit lights, and luminescent exit signs.

Battery powered exit lights are located at each entry door.

1.40.6A


Escape path-lighting consists of floor mounted photoluminescent strips alongthe aisle and exit indicators by each door. When illuminated, escape pathlighting provides visual guidance for emergency evacuation if all sources oflighting more than four feet above the aisle floor are obscured by smoke.

757SC-FCOM-01


Cargo Door Area LightsFour cargo lights are installed above the Main Cargo Door, and two on each sideof the door opening. The lights are enabled when the door is unlatched.

December 02, 2011


Systems Description

1.40.7A


Doors and WindowsThe airplane has four entry doors, two emergency doors, one flight deck door(the flight deck/courier area entry), one rigid cargo barrier door, one smoke

It also has electrical equipment and forward

The flight deck number two windows, one on the left and one on the right, can be opened by the flight crew.

An EICAS message is displayed when an entry door, emergency door, cargodoor or access door is not closed, and latched, and locked.

757SC-FCOM-01

barrier door and three cargo doors.equipment bay access doors.

Do not operate the entry and cargo doors with winds at theCAUTION:door of more than 40 knots. Do not keep the door open whenwind gusts are more than 65 knots (60 knots for Main Cargo

airplane.Door). Strong winds can cause damage to the structure of the



1.40.9A

Rigid Cargo Barrier DoorThe rigid cargo barrier (RCB) door is used to enter the main deck cargocompartment from the courier area and vice versa. The RCB door is a slidingtype and can be opened or closed manually from both sides. The RCB door hasa vent panel that relieves pressure in both directions above a pre-determined


Smoke Barrier DoorThe smoke barrier door is used to enter the main deck cargo compartment fromthe passenger cabin and vice versa. The smoke barrier door is a hinged type anddesigned to only open aftwards. Door handles to facilitate the opening andclosing of the smoke barrier door are found on both sides of this door. Duringflight, the smoke barrier door will be locked with a key held by the cabin crew.When closed, the smoke barrier door prevents leakage of smoke and halon gasesfrom the main deck cargo compartment to the passenger cabin.

757SC-FCOM-01

pressure differential.



1.40.12A


757SC-FCOM-01

Evacuation Slides



Systems Description

1.40.13A

The CARGO DOORS light illuminates and the EICAS advisory message FWD or AFT CARGO DOOR displays when the forward or aft cargo door is not closedand latched and locked. The EICAS advisory message CARGO DOORSdisplays if both forward and aft cargo doors are not closed and latched and

EICAS advisory message MAIN CARGO DOOR displays when the main cargodoor is not closed and latched and locked.


Cargo DoorsThere are three cargo doors; one main, one forward and one aft. The forward andaft doors are located on the right side of the airplane. The main door is located

Both forward and aft cargo doors are normally operated electrically from an exterior or interior fuselage–mounted control panel located with each door.

accomplished manually. If necessary, the main, forward and aft cargo doorsmay be operated manually.

on the left side of the airplane. The cargo doors open upward and outward.

The main deck cargo door is normally operated and locked from a panelmounted on the rigid cargo barrier. Forward and aft cargo door locking is

757SC-FCOM-01

locked. The MN CARGO DOOR and CARGO DOORS lights illuminate and



Emergency Equipment

Emergency Equipment Symbols

1.45.3A


757SC-FCOM-01

SPARE BULBKIT

SBK

KITFLARE

NOTE: Some symbols do not apply

FIRST AIDKIT

RESUSCITATORMEDICAL KITEMERGENCYFLASHLIGHTHANDCUFFSBATON

MEGAPHONECRASHAXE

INOP DOORKIT

SMOKEGOGGLES

PROTECTIVEGLOVES

LIFEVEST

ELT

ROPE

LIFE RAFTEXIT PATHWITH

SLIDE/RAFT

EXIT PATHWITH ESCAPE

SLIDE AND WITH ESCAPE

EXIT PATH

SLIDEROPE

EXIT PATHWITH ESCAPE

PRY BAREXTINGUISHER

HALONWATEREXTINGUISHER

WITH MASKOXYGEN BOTTLE

PORTABLE

S

SLIDE/RAFTSURVIVAL KIT

K

PORTABLEOXYGEN BOTTLE

CO2EXTINGUISHER

EMERGENCYEXIT PATH

SMOKEHOOD

EQUIPMENT

PORTABLEBREATHING

(PBE)

to all con�gurations.A = Attendant Station

GAL = GalleyLAV = Lavatory

P = Purser Station

CLO = Closet= Overhead Storage Bin

CO

2

NOTE: ("n") below symbol means quantity greater than one.

= Ceiling Storage

O2

H

LAH

2O O

2

IDK

DANGEROUSKIT

DGK

HEAT RESISTANTGLOVES

CHEMICALGLOVES

MASK

SBE

D/K

DEMOKIT

SEAT BELTEXT

SPAREMASKS

MANUALRELEASE

MRT

TOOL


Airplane General, Emergency Equipment, Doors, Windows -Emergency Equipment

Emergency Equipment Locations

1.45.4A


757SC-FCOM-01 December 23, 2011


OO-TFAAT EACH

CREW STATIONFLIGHT DECK

LAV

AA

GAL

LAV GAL

HAL

(2)

H2

OHAL

SBK

AT EACHPASSENGER SEAT

UNDER EACHATTENDANTSTATION

D/K

LAV

MRT

S

K

A

D/K

O2

(2)

SK

(2)

O2

(2)

(2)

HAL

O2

(2)

IDK

(5)

SBE

INFANT

(5)(5)(5)

SPARESEAT BELTS

(5)

KANGAROOBELT

CHILD

HAL

A

DGK

MRT

(2)

(2)

SK

(2)

Chapter 1Airplane General, Emergency Equipment, Doors, WindowsEICAS Messages Section 50

1.50 Airplane General, Emergency Equipment, Doors, Windows-EICAS MessagesAirplane General, Emergency Equipment, Doors, Windows EICAS MessagesThe following EICAS messages may be displayed.

Cargo DoorsMessage Level Light Aural Condition

1.50.1A

CARGOMain Cargo door is notclosed, latched and

DOOR locked.


757SC-FCOM-01

CARGODOORS

MAIN CARGO DOOR


Caution MN

(red)

August 28, 2012

Air Systems Chapter 2Table of Contents Section 0

2.TOC.0.1A

Courier Area Heaters


757SC-FCOM-01

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.20.3A

Courier Area Temperature Control . . . . . . . . . . . . . . . . . . . . . . . 2.10.10A


Controls and Indicators . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.10

Air Conditioning System Description . . . . . . . . . . . . . . . . . . . . . . 2.20

December 02, 2011


Air Systems Chapter 2Controls and Indicators Section 10

2.10 Air Systems-Controls and IndicatorsAir Conditioning System

Air Conditioning Control Panel

OVERHEAD PANEL

YBTS

W

NAUTO

OFF

RESETR PACK

RESETL PACK

FANTRIM AIR

WOFFCOFF WOFFCWC

AUTOAFT CAB

AUTOFWD CAB

AUTOFLT DK

OFFOFFPACKPACK

INOPINOP

ONINOP

INOP

ON

OFF INOP

COMPT TEMP

INOPINOP

L RECIRC

YBTS

W

NAUTO

OFF

9

10

12

1

2

3

4

5

6

78

DEAC

T

DEAC

T

2.10.1A757SC-FCOM-01

AFTCOUR/FWDFLT DK

INOP

11


Air Systems -Controls and Indicators


2.10.3A757SC-FCOM-01

STBY–• N (normal) – regulates the pack outlet temperature to a constant, moderate

temperature

• W (warm) – sets the pack to full warm operation.

10 Left Recirculation Fan (L RECIRC FAN) Switch• ON – the left recirculation fan operates• Off (ON not visible) – the left recirculation fan does not operate.

11 Left Recirculation Fan Inoperative (INOP) Light

Illuminated (amber) –• the left recirculation fan is failed or not operating• the L RECIRC FAN switch is off.

Note: Only the left recirculation fan is operable, the right recirculation fan isremoved on the combi freighter.

12 Inoperative (INOP) on combi freighter

• C (cool) – Deactivated on combi freighter


Courier Area Temperature Control

1 HEATER Switch• HIGH – the electric heater adds heat at high setting to the conditioned air

flowing to the courier area.• LOW – the electric heater adds heat at low setting to the conditioned air

• OFF – the electric heater is not operating (no heat added to the conditioned

2 TEMP IND Switch• FWD CABIN – Displays actual temperature sensed in the forward cabin in

the middle temperature indicator.• COURIER – Displays actual temperature sensed in the courier area in the

flowing to the courier area.

air flowing to the courier area).

middle temperature indicator.

OVERHEAD PANEL

1 2

TEMP IND

FWDCOURHIGHOFF

HEATER

LOW

INOP

INOP

COURIER

Air Systems -Controls and Indicators


2.10.10A757SC-FCOM-01


Air Systems Chapter 2Air Conditioning System Description Section 20

2.20 Air Systems-Air Conditioning System DescriptionAir Conditioning Standby ModeWith the pack selector in the standby mode, pack output temperature is determined by the position of the pack selector:

• N (normal) – constant, moderate temperature

• W (warm) – full warm.


2.20.1A757SC-FCOM-01

• C (cool) – deactivated


Air Systems -Air Conditioning System Description

Air DistributionConditioned air from the packs flows into a mix manifold where it mixes with air from the left recirculation fan. The right recirculation fan has been removed. The

main deck.

The flight deck receives 100% fresh conditioned air from the left pack only and is maintained at a slightly higher pressure than the main deck. This prevents smoke from entering the flight deck. When the left pack is inoperative, the flight deck receives air from the mix manifold.

The left recirculation fan draws air through the forward E/E system and returns it to the mix manifold. Air from the main cargo compartment is drawn into the mixbay by the cabin exhaust fan. Air from the passenger compartment exits into the

During normal operation, the left recirculation fan should not be turned off as thiscauses the overboard exhaust valve to latch open while airborne. Maintenance

left recirculation fan channels the air back to the mix manifold and thereby helps

action is required to reset this valve.


2.20.2A 757SC-FCOM-01

lower deck and exhausts overboard through the outflow valve.

The left recirculation fan INOP light illuminates and the EICAS advisorymessage L RECIR FAN displays whenever the left recirculation fan fails or theswitch is off. A slight increase in fuel consumption occurs if the fan is off.

The cabin exhaust fan draws main cargo compartment air into the mix manifoldbay via air plenums. When fire is detected in the main cargo compartment, thecabin exhaust fan will be turned off and its air shutoff valve will close to preventsmoke or halon gases to escape into the mix manifold bay.

to reduce the bleed air load on the engines. The mixed air is then ducted into the


Air Systems -Air Conditioning System

Description

Temperature ControlThe airplane is divided into three primary temperature control compartments:

• flight deck (FLT DK)• main cargo area (FWD CAB)• passenger compartment (AFT CAB)

The pack controllers regulate the pack output air temperature to satisfy the temperature requirement of the compartment requiring the coolest air. Hot trim air from the bleed air system is added through trim air valves to control the temperature in each of the other compartments. Each temperature control compartment has an associated temperature control.A compartment INOP light illuminates and the EICAS advisory message FLT DECK TEMP, FWD CABIN TEMP, or AFT CABIN TEMP displays to indicate

• zone temperature controller failure• zone selector is in the OFF position• trim air switch is OFF

Courier Area HeatersTwo courier area heaters are used to warm up the air for the comfort of thesupernumeraries.The Courier Heater Temperature Control Switch located on the CourierCommunication and Temperature Control Panel at the P5 Overhead Panel haspositions OFF, LOW and HIGH to allow pilot/co-pilot to adjust heat outputmanually.


2.20.3A757SC-FCOM-01

any of the following conditions:


Air Systems -Air Conditioning System Description

Equipment Smoke


2.20.4A 757SC-FCOM-01

Note: Only the left recirculation fan is enabled, the rightrecirculation fan is removed on the combi freighter.



Air Systems -Air Conditioning System

Description

Air Conditioning System Schematic

OFFOFFC C

AFT CABAUTO

FWD CABAUTO

PACKOFF

INOP

INOP

COMPT TEMP

INOP INOP

RESET

R PACKL PACK

TRIM AIR

RESET

L RECIRCFAN

MIX MANIFOLD

PNEUMATICSUPPLY

PNEUMATICSUPPLY

AUTOOFF N

W

STBY

AUTOOFF N

W

STBY

AIR

PACK AIR

EXHAUST AIR

MIX MANIFOLD

TRIM AIR

PACKOFF

INOP

OFFC

FLT DKAUTO

INOPON

INOP

ON

OFF

WWW

2.20.5A

DEAC

T

DEAC

T

757SC-FCOM-01

INOP

COMPT TEMP

FLT DK COUR/FWD AFT


Fire Protection Chapter 8Table of Contents Section 0

8.0 Fire Protection-Table of Contents

Controls and Indicators . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.10

System Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.20

Cargo Compartment Fire Protection . . . . . . . . . . . . . . . . . . . . . . 8.20.4


Main Deck Cargo Compartment Alarm Panel . . . . . . . . . . . . . . 8.10.3B

8.TOC.0.1A757SC-FCOM-01

Main Deck Cargo Compartment Fire Warning . . . . . . . . . . . . 8.20.4AMain Deck Cargo Compartment Fire Extinguishing . . . . . . . . 8.20.5A


Main Deck Cargo Compartment Fire Panel . . . . . . . . . . . . . . . . 8.10.3A

Main Deck Cargo Compartment Fire Suppression Panel . . . . . . 8.10.3B

December 02, 2011


Fire Protection -Controls and Indicators

Main Deck Cargo Compartment Fire Panel

1 Main Deck Smoke Detector Loop SwitchRotate - either loop A, loop B or BOTH loops.

RIGHT OVERHEAD PANEL

2 Main Deck Smoke Detector Fault Light

zone.

1 Main Deck FIRE Warning LightIlluminated (red) - smoke is detected in the associated zone.

3

4 SYSTEM TEST SwitchPush - initializes a test sequence for the main deck smoke detection system.

Illuminated (amber) - fault is detected in the smoke detection system for that

1

2

3

4

8.10.3A757SC-FCOM-01

SYSTEM

FAULT

FWDBOTH

A B

FIRE

MAIN

FAULT

BOTHA B

FIRE

MIDBOTH

A B

DEACTTEST

IRE

FDEACT


DEACT

DEACT

December 02, 2011

Fire Protection -



Main Deck Cargo Compartment Alarm Panel

1 ALARM OFF SWITCH

OVERHEAD PANEL

1

Push - silences the main deck cargo compartment fire alarm.

1 MAIN CARGO FIRE SUPPRESSION ARM SwitchROTATE

• arms the main deck cargo compartment fire extinguisher bottles.

• shuts off airflow and isolates the main deck cargo compartment.

8.10.3B 757SC-FCOM-01

ALARMOFF

4

52

RIGHT OVERHEAD PANEL

ARMEDOFF

SYS TEST

BTL

DSCH

BTL

3 54

1 2

1

Main Deck Cargo Compartment Fire Suppression Panel


MAIN CARGO SMOKE ALARM

3

MAIN CARGO FIRESUPPRESSION

ARM

FIRE

BTL DSCH

December 02, 2011


Fire Protection -Controls and Indicators

8.10.3C757SC-FCOM-01

2 MAIN CARGO FIRE SUPPRESSION SYS TEST SwitchPush - illuminates the fire extinguisher bottle lights 1 - 5 (green) and the DSCH

3 Main Deck Cargo Compartment FIRE Warning Light

1

Push - discharges the fire extinguisher bottles into the main deck cargo

4

5 MAIN DECK FIRE SUPPRESSION Bottle (BTL) Ready Lights

Illuminated (red) - smoke is detected in the main deck cargo compartment

light (amber).

MAIN CARGO FIRE SUPPRESSION Bottle Discharge (BTL DSCH)Switch

compartment.

Illuminated (green) - the associated extinguisher bottle is armed and ready for

Illuminated (amber) - fire extinguishing agent is being discharged into the maindeck cargo compartment.

discharge.


Fire Protection -System Description

Cargo Compartment Smoke DetectionThe forward, aft and main deck cargo compartment(s) each have smoke

The SYS FAIL light illuminates and the EICAS advisory message FIRE/OVHT SYS displays to indicate failure of the forward and aft cargo compartment smokedetection system. The SYS FAIL light can be reset to allow monitoring of the remaining systems.The FAULT light illuminates and the EICAS advisory message FIRE/OVHT

smoke detection system for the associated zone. Selecting the zone loop switchto either A or B can reset the fault light when the operational loop is selected.The corresponding zone will operate in a single loop.


8.20.4A 757SC-FCOM-01

Main Deck Cargo Compartment Fire WarningThe indications of a main cargo compartment fire warning are:

• the main cargo fire alarm sounds

Compartment Fire Panel illuminates.

Unit illuminates.The fire warning lights remain illuminated until smoke is no longer detected. Thefire alarm may be silenced by any of the following actions:

• extinguishing the fire and clearing the smoke

Panel illuminates.

• pushing either master warning/caution reset switch• pushing the ALARM OFF button on the MAIN CARGO SMOKE ALARM

• the master WARNING lights illuminate• the discrete FIRE warning light illuminates• MAIN CARGO FIRE message is displayed on the EICAS• the appropriate FWD or MID FIRE indication on the Main Deck Cargo

• FIRE Warning light on the Main Deck Cargo Compartment Fire Suppression

• the corresponding LED indicator for the detector on the Cargo Electronic

detectors installed.

SYS displays on the main smoke panel to indicate failure of the main deck


panel.

December 02, 2011

Fire Protection -System Description

Main Deck Cargo Compartment Fire Extinguishing


8.20.5A757SC-FCOM-01

Fire extinguisher bottles are installed for main cargo compartment fireextinguishing.

Rotating the main deck fire suppression panel ARM switch to ARMED theextinguishers for the compartment. This action cuts off air into and out of the main deck cargo compartment. In addition, the arming action turns off the forward lower lobe cargo compartment's heater and its fan.

Alternate cooling to the E/E bay will be provided from the mix manifold.

Pushing the bottle discharge (BTL DSCH) button on the main deck firesuppression panel will activate the high rate discharge of the halon agent fromfire extinguisher bottles 1 and 2. After 20 minutes, the low rate discharge ofthe halon agent from fire extinguisher bottles 3, 4 and 5 will be automaticallyactivated to maintain the required concentration.


Fire Protection Chapter 8System EICAS Messages Section 30

8.30 Fire Protection-System EICAS MessagesFire Protection EICAS Messages

Message Level Light Aural Condition

MAIN CARGO FIRE Wor MID)

Fire Alarm

Smoke is detected in themain cargo compartment


8.30.1A757SC-FCOM-01

arning FIRE (FWD


Hydraulics Chapter 13Table of Contents Section 0

13.0 Hydraulics-Table of Contents

System Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13.20

Left Hydraulic System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13.20.3Hydraulic Pressure For Main Cargo Door . . . . . . . . . . . . . . . 13.20.4A


13.TOC.0.1A757SC-FCOM-01


Hydraulics Chapter 13System Description Section 20

13.20 Hydraulics-System DescriptionIntroductionThe airplane has three independent hydraulic systems: left, right, and center. The hydraulic systems power the:

• flight controls• leading edge slats• trailing edge flaps• landing gear• wheel brakes• nose wheel steering• thrust reversers• autopilot servos


13.20.1A757SC-FCOM-01

• main cargo door (ground only)

Flight control system components are distributed so that any one hydraulicsystem can provide adequate airplane controllability.Hydraulic fluid is supplied to each hydraulic pump from the associated systemreservoir. The reservoirs are pressurised by the bleed air system.


Hydraulics -System Description

Hydraulic Systems Schematic

FLT CTRL

L REV

POWER TRANSUNIT (PTU)

FLT CTRL

R REV

NORM BRKS

ENG

ELECELEC

SOVSOV

LEFT CENTER RIGHT

ENG

ELEC ELEC RAT

ISLNSOV

L

LC1 C2

R

R

FLAPS

SLATSHYD DRIVENGENERATOR

NOSE WHEELSTEERING

LND GEAR

FLT CTRL

ISLN

SHUTOFFVALVE

ISOLATIONVALVE

PUMP

LEFT

DISCH21

ALTN BRAKES

RESERVOIRRESERVOIR RESERVOIR

HYD

ENGR

- 2ELEC1C

ENGL

PUMPS

ELECELEC

-

PRESS

ON

PRESS

ON

PRESS

ON

PRESS

ON

PRESS

ON

PRESS

ON

OVHTOVHT

OVHTOVHTOVHTOVHT

RAM AIR TURB

UNLKD

PRESS

RESERVEBRAKES

ON

MAIN CARGODOOR


13.20.2A 757SC-FCOM-01



Left Hydraulic SystemThe left hydraulic system powers:

• flight controls• flaps and slats• landing gear• alternate brakes• nose wheel steering• left engine thrust reverser• hydraulic driven generator

The system consists of a reservoir, engine–driven pump, electric motor–driven pump, and a power transfer unit (PTU) pump.


13.20.3A757SC-FCOM-01

• main cargo door (ground only)



Hydraulic Pressure for Main Cargo DoorHydraulic pressure is supplied to the main cargo door through a shutoffvalve when the nose and main landing gear are in the down position and supporting the weight of the airplane.


13.20.4A 757SC-FCOM-01


Warning Systems -System Description

Configuration Alerts757 Flight Crew Operations Manual Supplement

15.20.10A 757SC-FCOM-01

Note: Takeoff configuration warning messages includes MAINCARGO DOOR on the combi freighter.


Warning Systems -EICAS Messages

Message Level Light Aural Condition

DOOR (discrete closed, latched and locked when either engine's thrust is in the takeoff range on the ground.


15.30.2A 757SC-FCOM-01

MAIN CARGO Warning CONFIG Siren Main Cargo Door is not

Configuration

light - No EICASMESSAGE)


MNCARGODOOR

December 02, 2011

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